| 液化气体推进剂在微小卫星推进系统中的应用 |
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| 引用本文： | 马彦峰,边炳秀.液化气体推进剂在微小卫星推进系统中的应用[J].空间控制技术与应用,2008,34(2):59-64. |
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| 作者姓名： | 马彦峰 边炳秀 |
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| 作者单位： | 北京控制工程研究所,北京,100190 |
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| 摘 要： | 随着微小型卫星的发展，液化气推进系统成为了此类航天器推进系统的选择。目前，国内外常用的液化气推进剂有一氧化二氮、丁烷、丙烷、氨等。本文对液化气推进剂的发展历史和研究现状进行了综述，对液化气推进系统在应用中面临的技术问题进行了分析，并在综合考虑各项因素的情况下，推荐采用一氧化二氮作为微小卫星液化气推进系统的推进剂。
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| 关 键 词： | 微小卫星 推进系统 液化气体推进剂 |
Application of Liquefied Gas Propellants in Micro Satellite Propulsion Systems |
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| MA Yanfeng,BIAN Bingxiu.Application of Liquefied Gas Propellants in Micro Satellite Propulsion Systems[J].Aerospace Contrd and Application,2008,34(2):59-64. |
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| Authors: | MA Yanfeng BIAN Bingxiu |
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| Abstract: | The liquefied gas propulsion system is a good selection for the micro satellite orbit and attitude control.In the past 30 years,several kinds of liquefied gases were used as the propellant in micro satellites,including nitrous oxide,butane,propane and ammonia.In this paper,a general development of liquefied gas propellants is introduced,especially nitrous oxide is recommended as a propellant of liquefied gas propulsion systems for micro satellites. |
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| Keywords: | micro satellite propulsion system liquefied gas propellant |
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